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  2. DO-178B - Wikipedia

    en.wikipedia.org/wiki/DO-178B

    DO-178B, Software Considerations in Airborne Systems and Equipment Certification is a guideline dealing with the safety of safety-critical software used in certain airborne systems. It was jointly developed by the safety-critical working group RTCA SC-167 of the Radio Technical Commission for Aeronautics (RTCA) and WG-12 of the European ...

  3. DO-178C - Wikipedia

    en.wikipedia.org/wiki/DO-178C

    Download QR code ; Print/export ... and boundaries between the key DO-178B concepts of high-level requirements, ... and derived requirements and a better definition ...

  4. Integrity (operating system) - Wikipedia

    en.wikipedia.org/wiki/Integrity_(operating_system)

    INTEGRITY-178B is the DO-178B–compliant version of INTEGRITY. It is used in several military jets such as the B-2, [2] F-16, F-22, and F-35, and the commercial aircraft Airbus A380. [3] Its kernel design guarantees bounded computing times by eliminating features such as dynamic memory allocation.

  5. CAST-15 - Wikipedia

    en.wikipedia.org/wiki/CAST-15

    CAST-15, Merging High-Level and Low-Level Requirements is a Certification Authorities Software Team (CAST) Position Paper. It is an FAA publication that "does not constitute official policy or guidance from any of the authorities", but is provided to applicants for software and hardware certification for educational and informational purposes only.

  6. AC 20-115 - Wikipedia

    en.wikipedia.org/wiki/AC_20-115

    The earliest revisions of the Advisory Circular were brief, serving little more than to call attention to active DO-178 revisions. The Advisory Circular revisions C and D are considerably longer, giving guidance in modifying and re-using software previously approved using DO-178, DO-178A, or DO-178B (preceding revisions of the DO-178 standard).

  7. MIL-STD-498 - Wikipedia

    en.wikipedia.org/wiki/MIL-STD-498

    MIL-STD-498 standard describes the development and documentation in terms of 22 Data Item Descriptions (DIDs), which were standardized documents for recording the results of each the development and support processes, for example, the Software Design Description DID was the standard format for the results of the software design process.

  8. Modified condition/decision coverage - Wikipedia

    en.wikipedia.org/wiki/Modified_condition/...

    MC/DC is used in avionics software development guidance DO-178B and DO-178C to ensure adequate testing of the most critical (Level A) software, which is defined as that software which could provide (or prevent failure of) continued safe flight and landing of an aircraft.

  9. Certification Authorities Software Team - Wikipedia

    en.wikipedia.org/wiki/Certification_Authorities...

    The Certification Authorities Software Team (CAST) is an international group of aviation certification and regulatory authority representatives. The organization of has been a means of coordination among representatives from certification authorities in North and South America, Europe, and Asia, in particular, the FAA and EASA.